Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages VI : over-all performance, rotating stall, and blade vibration at low and intermediate compressor speeds

Author:	Standahar, Raymond M
Additional Authors:	Hanson, Morgan P
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E55I13
Link:	https://digital.library.unt.edu/ark:/67531/metadc61596/